Multi-piece solid golf ball

ABSTRACT

In a multi-piece solid golf ball comprising a solid core, a mantle and a cover, the solid core is made of a rubber composition that includes a base rubber containing a polybutadiene synthesized using a rare-earth catalyst, a small amount of organic peroxide, an unsaturated carboxylic acid and/or a metal salt thereof, an organic sulfur compound and an inorganic filler. The mantle is made of a thermoplastic resin composition. The cover is made primarily of a mixture containing an amino-terminated block polymer and an ionomer resin. This construction provides the golf ball with a combination of outstanding flight performance, excellent scuff resistance and soft feel that is unprecedented.

BACKGROUND OF THE INVENTION

1. Field of the Invention

The present invention relates to golf balls which have an outstandingflight performance, an excellent scuff resistance and a soft “feel” uponimpact.

2. Prior Art

Golf balls have hitherto been modified and improved in a variety of waysto address the numerous and diverse requirements of golfers. The presentassignee, among others, has already disclosed many outstanding golfballs.

For example, JP-A 9-313643 describes an all-round golf ball which hasexcellent flight characteristics and durability, a good, soft feel onimpact, and controllability.

JP-A 10-305114 discloses a golf ball having a dramatically increasedcarry and a good feel on impact.

JP-A 11-114094 teaches a golf ball in which deflection by the solid coreand the relative thicknesses and hardnesses of the cover and the mantlehave been optimized so to provide a good trajectory and increased carryon shots with a driver, suitable spin characteristics and goodcontrollability on approach shots, excellent feel on impact andexcellent durability.

JP-A 2000-225209 relates to golf balls with an excellent overallperformance that have the feel, durability and rebound characteristicsrequired of a ball construction subject to limitations with respect tosolid core deformation, hardness of the cover and the mantle and dimplecharacteristics, and that also have excellent flight characteristics.

JP-A 2001-218873 describes a golf ball of outstanding feel,controllability and flight performance—including carry, in which themantle and/or cover are formed of specific materials, and in which therespective Shore D hardnesses of the solid core center and surface andof the mantle and the cover are such as to satisfy the followingrelationship: solid core center hardness≦mantle hardness≦cover hardness.

JP-A 2002-210042 discloses a golf ball having a very soft feel on impactyet good durability and also having a low spin, high angle of elevationand high rebound that together provide increased carry. This prior-artgolf ball is achieved by specifying all of the following: centerhardness, surface hardness and diameter of the solid core, mantlehardness, thickness and material, cover hardness, thickness andmaterial, difference in hardness between mantle and solid core surface,difference in hardness between cover and mantle, relationship betweenhardness gradient from mantle to cover and hardness gradient from centerof core to mantle, and dimple arrangement.

JP-A 8-276033 teaches a way of obtaining a solid golf ball having a goodfeel on impact and a long carry by setting the difference A−B betweenthe compression deflection A by the core when subjected to a final loadof 130 kgf from an initial load of 10 kgf and the compression deflectionB by the ball when subjected to a final load of 130 kgf from an initialload of 10 kgf within a specific range.

These prior-art golf balls all have an excellent feel and an excellentcarry and other flight characteristics, and can be suitably adapted tovarious requirements dictated by the skill level of the golfer and theintended use of the ball (e.g., recreational or competitive). Yet, giventhe ever-high expectations of golfers, there exists a need for golfballs endowed with an even better performance.

SUMMARY OF THE INVENTION

It is therefore an object of the present invention to provide golf ballswhich have excellent flight characteristics and scuff resistance, andwhich also have a soft feel on impact.

We have found that multi-piece solid golf balls constructed of a solidcore, a mantle of at least one layer and a cover can be conferred withbetter flight characteristics, a higher scuff resistance and a softerfeel on impact than prior-art golf balls by having the solid core madeof a specific rubber composition and endowed with a specific degree offlexibility and diameter, having the mantle made of a specificthermoplastic resin composition and endowed with a specific thicknessand hardness, having the cover made of a specific resin composition andendowed with a specific thickness and hardness, and setting theflexibility of the overall golf ball within a specific range.

Accordingly, this invention provides a multi-piece solid golf ballconstructed of a solid core, a mantle of at least one layer whichencloses the core, and a cover which encloses the mantle, wherein thesolid core is made of a rubber composition comprising (A) 100 parts byweight of a base rubber that contains 60 to 100 wt % of a polybutadieneof at least 60% cis-1,4 structure and synthesized using a rare-earthcatalyst, (B) 0.1 to 0.8 part by weight of an organic peroxide, (C) anunsaturated carboxylic acid and/or a metal salt thereof, (D) an organicsulfur compound and (E) an inorganic filler, has a deflection whensubjected to a load of 980 N (100 kgf) of 3.0 to 6.0 mm, and has adiameter of 30 to 40 mm; the mantle of at least one layer is made of athermoplastic resin composition, has a thickness per layer of 0.5 to 2.0mm, and includes an outermost layer which is in contact with the coverand has a Shore D hardness of 20 to 60; the cover is composed primarilyof a mixture of (M) an amino-terminated block polymer and (N) an ionomerresin in a weight ratio M/N of 3/97 to 60/40, has a thickness of 0.5 to2.5 mm, has a Shore D hardness of 50 to 70, and satisfies the condition(Shore D hardness of mantle outermost layer)≦(Shore D hardness ofcover); and the golf ball has a deflection when subjected to a load of980 N (100 kgf) of 3.0 to 5.0 mm.

The polybutadiene is typically a modified polybutadiene prepared bysynthesis using a neodymium catalyst, followed by reaction with aterminal modifier.

Preferably, the rubber composition includes (A) 100 parts by weight of abase rubber containing 60 to 100 wt % of a polybutadiene of at least 60%cis-1,4 structure and synthesized using a rare-earth catalyst, (B) 0.1to 0.8 part by weight of at least two kinds of organic peroxide, (C) 10to 60 parts by weight of an unsaturated carboxylic acid and/or a metalsalt thereof, (D) 0.1 to 5 parts by weight of an organic sulfurcompound, and (E) 5 to 80 parts by weight of an inorganic filler.

The thermoplastic resin composition making up the mantle is preferablycomposed of 100 parts by weight of resin components which include a baseresin of (P) an olefin/unsaturated carboxylic acid binary randomcopolymer and/or a metal ion neutralization product of anolefin/unsaturated carboxylic acid binary random copolymer in admixturewith (Q) an olefin/unsaturated carboxylic acid/unsaturated carboxylicacid ester ternary random copolymer and/or a metal ion neutralizationproduct of an olefin/unsaturated carboxylic acid/unsaturated carboxylicacid ester ternary random copolymer in a weight ratio P/Q of 100:0 to25:75, and (R) a non-ionomeric thermoplastic elastomer in a weight ratio(P+Q)/R of 100:0 to 50:50; (S) 5 to 80 parts by weight of a fatty acidor/or fatty acid derivative having a molecular weight of 280 to 1,500;and (T) 0.1 to 10 parts by weight of a basic inorganic metal compoundcapable of neutralizing un-neutralized acid groups in the base resin andcomponent S.

Preferably, the mantle consists of an inner layer and an outer layer.

Typically the golf ball cover bears a plurality of dimples on a surfacethereof. Each dimple has a spatial volume below a planar surfacecircumscribed by an edge of the dimple and having a surface areacircumscribed by the dimple edge on a hypothetical sphere represented bythe surface of the golf ball cover were it to have no dimples. It ispreferable for the golf ball to have a dimple volume occupancy VR,defined as the ratio of the sum of the individual dimple volumes to thevolume of the hypothetical sphere, of 0.70 to 1.00%, and a dimplesurface coverage SR, defined as the ratio of the sum of the individualdimple surface areas to the surface area of the hypothetical sphere, of70 to 85%.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1 shows exemplary arrangements of dimples of sets A and C in Table4 on golf balls.

FIG. 2 shows exemplary arrangements of dimples of set B in Table 4 ongolf balls.

DETAILED DESCRIPTION OF THE INVENTION

The solid core in the golf ball of the invention is made of a rubbercomposition which includes:

(A) a base rubber that contains 60 to 100 wt % of a polybutadiene of atleast 60% cis-1,4 structure and synthesized using a rare-earth catalyst,

(B) an organic peroxide,

(C) an unsaturated carboxylic acid and/or a metal salt thereof,

(D) an organic sulfur compound, and

(E) an inorganic filler.

In component A, which is a base rubber that contains 60 to 100 wt % of apolybutadiene of at least 60% cis-1,4 structure and synthesized using arare-earth catalyst, the content of cis-1,4 units in the polybutadieneis at least 60%, preferably at least 80%, more preferably at least 90%,and most preferably at least 95%. At a cis-1,4 unit content of less than60%, suitable resilience is not achieved.

The polybutadiene in the invention is synthesized using a rare-earthcatalyst. A known rare-earth catalyst may be used for this purpose.Exemplary catalysts include lanthanide series rare-earth compounds incombination with organoaluminum compounds, alumoxanes, halogen-bearingcompounds or Lewis bases.

Examples of suitable lanthanide series rare-earth compounds includehalides, carboxylates, alcoholates, thioalcoholates and amides of atomicnumber 57 to 71 metals.

Organoaluminum compounds that may be used include those of the formulaAlR¹R²R³ (wherein R¹, R² and R³ are each independently a hydrogen or ahydrocarbon residue of 1 to 8 carbons).

Preferred alumoxanes include compounds of the structures shown informulas (I) and (II) below. The alumoxane association complexesdescribed in Fine Chemical 23, No. 9, 5 (1994), J. Am. Chem. Soc. 115,4971 (1993), and J. Am. Chem. Soc. 117, 6465 (1995) are also acceptable.

In the above formulas, R⁴ is a hydrocarbon group having 1 to 20 carbonatoms, and n is 2 or a larger integer.

Examples of halogen-bearing compounds that may be used include aluminumhalides of the formula AlX_(n)R_(3−n) (wherein X is a halogen; R is ahydrocarbon residue of 1 to 20 carbons, such as an alkyl, aryl oraralkyl; and n is 1, 1.5, 2 or 3); strontium halides such as Me₃SrCl,Me₂SrCl₂, MeSrHCl₂ and MeSrCl₃ (wherein “Me” stands for methyl); andother metal halides such as silicon tetrachloride, tin tetrachloride andtitanium tetrachloride.

The Lewis base can be used to form a complex with the lanthanide seriesrare-earth compound. Illustrative examples include acetylacetone andketone alcohols.

In the practice of the invention, the use of a neodymium catalyst inwhich a neodymium compound serves as the lanthanide series rare-earthcompound is advantageous because it enables a polybutadiene rubberhaving a high cis-1,4 unit content and a low 1,2-vinyl unit content tobe obtained at an excellent polymerization activity. Preferred examplesof such rare-earth catalysts include those mentioned in JP-A 11-35633.

To achieve a polybutadiene having a cis unit content within the aboverange and a desirable polydispersity Mw/Mn, the polymerization ofbutadiene in the presence of a rare-earth catalyst containing alanthanide series rare-earth compound is carried out at abutadiene/(lanthanide series rare-earth compound) molar ratio ofpreferably 1,000 to 2,000,000, and especially 5,000 to 1,000,000, and atan AlR¹R²R³/(lanthanide series rare-earth compound) molar ratio of 1 to1,000, and especially 3 to 500. It is also preferable for the (halogencompound)/(lanthanide series rare-earth compound) molar ratio to be 0.1to 30, and especially 0.2 to 15, and for the (Lewis base)/(lanthanideseries rare-earth compound) molar ratio to be 0 to 30, and especially 1to 10.

The polymerization of butadiene in the presence of a rare-earth catalystmay be carried out either in a solvent or by bulk polymerization orvapor phase polymerization without the use of solvent, and at apolymerization temperature in a range of generally −30° C. to 150° C.,and preferably 10 to 100° C.

The polybutadiene has a Mooney viscosity (ML₁₊₄ (100° C.)) of generallyat least 40, preferably at least 50, more preferably at least 52, andmost preferably at least 54, but generally not more than 140, preferablynot more than 120, more preferably not more than 100, and mostpreferably not more than 80. At a Mooney viscosity outside of the aboverange, the rubber composition may be more difficult to work and theresulting solid core may have a lower resilience.

The term “Mooney viscosity” used herein refers in each case to anindustrial index of viscosity (see JIS K6300) as measured with a Mooneyviscometer, which is a type of rotary plastometer. This value isrepresented by the symbol ML₁₊₄ (100° C.), wherein “M” stands for Mooneyviscosity, “L” stands for large rotor (L-type), and “1+4” stands for apre-heating time of 1 minute and a rotor rotation time of 4 minutes. The“100° C.” indicates that measurement was carried out at a temperature of100° C.

According to a preferred embodiment of the invention, the polybutadienemay be a modified polybutadiene obtained by polymerization using theabove-described rare-earth catalyst, followed by the reaction of aterminal modifier with active end groups on the polymer.

Any known terminal modifier may be used. Examples include terminalmodifiers of types (1) to (7) below.

(1) Alkoxysilyl group-bearing compounds, and preferably alkoxysilanecompounds having at least one epoxy group or isocyanate group on themolecule. Specific examples include epoxy group-bearing alkoxysilanessuch as

3-glycidyloxypropyltrimethoxysilane,

3-glycidyloxypropyltriethoxysilane,

(3-glycidyloxypropyl)methyldimethoxysilane,

(3-glycidyloxypropyl)methyldiethoxysilane,

β-(3,4-epoxycyclohexyl)trimethoxysilane,

β-(3,4-epoxycyclohexyl)triethoxysilane,

β-(3,4-epoxycyclohexyl)methyldimethoxysilane,

β-(3,4-epoxycyclohexyl)ethyldimethoxysilane, condensation products of3-glycidyloxypropyltrimethoxysilane and condensation products of

(3-glycidyloxypropyl)methyldimethoxysilane; and isocyanate group-bearingalkoxysilane compounds such as

3-isocyanatopropyltrimethoxysilane,

3-isocyanatopropyltriethoxysilane,

(3-isocyanatopropyl)methyldimethoxysilane,

(3-isocyanatopropyl)methyldiethoxysilane, condensation products of3-isocyanatopropyltrimethoxysilane and condensation products of

(3-isocyanatopropyl)methyldimethoxysilane.

A Lewis acid can be added to accelerate the reaction when the abovealkoxysilyl group-bearing compound is reacted with active end groups.The Lewis acid acts as a catalyst to promote the coupling reaction, thusimproving cold flow by the modified polymer and providing a better shelfstability. Examples of suitable Lewis acids include dialkyltin dialkylmalates, dialkyltin dicarboxylates and aluminum trialkoxides.

Other types of terminal modifiers that may be used include:

(2) halogenated organometallic compounds, halogenated metallic compoundsand organometallic compounds of the general formulas R⁵ _(n)M′X_(4−n),M′X₄, M′X₃, R⁵ _(n)M′(—R⁶—COOR⁷)_(4−n) or R⁵ _(n)M′(—R⁶—COR⁷)_(4−n)(wherein R⁵ and R⁶ are each independently a hydrocarbon group of 1 to 20carbons; R⁷ is a hydrocarbon group of 1 to 20 carbons which may containpendant carbonyl or ester groups; M′ is a tin, silicon, germanium orphosphorus atom; X is a halogen atom; and n is an integer from 0 to 3);

(3) heterocumulene compounds having on the molecule a Y═C═Z linkage(wherein Y is a carbon, oxygen, nitrogen or sulfur atom; and Z is anoxygen, nitrogen or sulfur atom);

(4) three-membered heterocyclic compounds containing on the molecule thefollowing bonds

 (wherein Y is an oxygen, nitrogen or sulfur atom);

(5) halogenated isocyano compounds;

(6) carboxylic acids, acid halides, ester compounds, carbonate compoundsand acid anhydrides of the respective formulas R⁸—(COOH)_(m),R⁹(COX)_(m), R¹⁰—(COO—R¹¹)_(m), R¹²—OCOO—R¹³ and R¹⁴—(COOCO—R¹⁵)_(m),and compounds of the formula

 (wherein R⁸ to R¹⁶ are each independently a hydrocarbon group of 1 to50 carbons, X is a halogen atom, and m is an integer from 1 to 5); and

(7) carboxylic acid metal salts of the formula R¹⁷ ₁M″(OCOR¹⁸)⁴⁻¹ or R¹⁹₁M″(OCO—R²⁰—COOR²¹)⁴⁻¹, and compounds of the formula

 (wherein R¹⁷ to R²³ are each independently a hydrocarbon group of 1 to20 carbons, M″ is a tin, silicon or germanium atom, and 1 is an integerfrom 0 to 3).

The above terminal modifiers and methods for their reaction aredescribed in, for example, JP-A 11-35633, JP-A 7-268132 and JP-A2002-293996.

Of the above catalysts, rare-earth catalysts, and especially neodymiumcatalysts, are especially preferred.

It is advantageous for the polybutadiene used in the invention to have apolydispersity index Mw/Mn (where Mw is the weight-average molecularweight, and Mn is the number-average molecular weight) of at least 2.0,preferably at least 2.2, more preferably at least 2.4, and mostpreferably at least 2.6, but not more than 8.0, preferably not more than7.5, more preferably not more than 4.0, and most preferably not morethan 3.4. If the polydispersity index Mw/Mn is too low, the rubbercomposition may be more difficult to work. On the other hand, if Mw/Mnis too large, the solid core may have a lower resilience.

In the practice of the invention, component A is a base rubber composedprimarily of the above-described polybutadiene. The polybutadienecontent within the base rubber is at least 60 wt %, preferably at least70 wt %, more preferably at least 80 wt %, and most preferably at least85 wt %. The content of the above polybutadiene in the base rubber maybe as much as 100 wt %, although the polybutadiene content can be set to95 wt % or less, or in some cases 90 wt % or less. At a polybutadienecontent within the base rubber of less than 60 wt %, the core has a poorresilience.

In addition to the above-described polybutadiene, the base rubberserving as component A may include also other polybutadienes, such aspolybutadienes prepared using a group VIII metal compound catalyst, andother diene rubbers, some examples of which are styrene-butadienerubber, natural rubber, isoprene rubber and ethylene-propylene-dienerubber.

Of the rubber ingredients other than the above-described polybutadiene,the use of a second polybutadiene prepared using a group VIII catalystand having a Mooney viscosity (ML₁₊₄ (100° C.)) of less than 50 and aviscosity η at 25° C., as a 5 wt % toluene solution, of at least 200mPa.s but not more than 400 mPa.s is preferable for achieving a highresilience and good workability.

Group VIII catalysts that may be used include nickel catalysts andcobalt catalysts.

Examples of suitable nickel catalysts include single-component systemssuch as nickel-kieselguhr, binary systems such as Raney nickel/titaniumtetrachloride, and ternary systems such as nickelcompound/organometallic compound/boron trifluoride etherate. Exemplarynickel compounds include reduced nickel on a carrier, Raney nickel,nickel oxide, nickel carboxylate and organonickel complex salts.Exemplary organometallic compounds include trialkylaluminum compoundssuch as triethylaluminum, tri-n-propylaluminum, triisobutylaluminum andtri-n-hexylaluminum; alkyllithium compounds such as n-butyllithium,sec-butyllithium, tert-butyllithium and 1,4-dilithiumbutane: anddialkylzinc compounds such as diethylzinc and dibutylzinc.

Examples of suitable cobalt catalysts include the following composed ofcobalt or cobalt compounds: Raney cobalt, cobalt chloride, cobaltbromide, cobalt iodide, cobalt oxide, cobalt sulfate, cobalt carbonate,cobalt phosphate, cobalt phthalate, cobalt carbonyl, cobaltacetylacetonate, cobalt diethyldithiocarbamate, cobalt anilinium nitriteand cobalt dinitrosyl chloride. It is particularly advantageous to usethese compounds in combination with, for example, a dialkylaluminummonochloride such as diethylaluminum monochloride or diisobutylaluminummonochloride; a trialkylaluminum such as triethylaluminum,tri-n-propylaluminum, triisobutylaluminum or tri-n-hexylaluminum; analkylaluminum sesquichloride such as ethylaluminum sesquichloride; oraluminum chloride.

Polymerization using the group VIII catalysts described above, andespecially a nickel or cobalt catalyst, can generally be carried out bya process in which the catalyst is continuously charged into the reactortogether with a solvent and the butadiene monomer. The reactionconditions are suitably selected from a temperature range of 5 to 60° C.and a pressure range of atmospheric pressure to 70 plus atmospheres, soas to yield a product having the above-indicated Mooney viscosity.

The second polybutadiene has a Mooney viscosity of less than 50,preferably no more than 48, and most preferably no more than 45. It isadvantageous for the lower limit in the Mooney viscosity to be at least10, preferably at least 20, more preferably at least 25, and mostpreferably at least 30.

The second polybutadiene has a viscosity η at 25° C., as a 5 wt %solution in toluene, of at least 200 mPa.s, preferably at least 210mPa.s, more preferably at least 230 mPa.s, and most preferably at least250 mPa.s, but not more than 400 mPa.s, preferably not more than 370mPa.s, more preferably not more than 340 mPa.s, and most preferably notmore than 300 mPa.s.

In the invention, the “viscosity η at 25° C. as a 5 wt % solution intoluene” (in mPa.s) refers to the value obtained by dissolving 2.28 g ofthe polybutadiene to be measured in 50 ml of toluene and using as thereference fluid a standard fluid for viscometer calibration (JIS Z8809)to carry out measurement at 25° C. with the requisite viscometer.

The second polybutadiene is typically included in the base rubber in anamount of 0% or more, preferably at least 5%, and more preferably atleast 10% by weight, but not more than 40%, preferably not more than30%, even more preferably not more than 20%, and most preferably notmore than 15% by weight.

It is preferable to use at least two kinds of organic peroxide ascomponent B in the invention. If (a) represents the organic peroxidehaving the shortest half-life at 155° C., (b) represents the organicperoxide having the longest half-life at 155° C., and the half-lives of(a) and (b) are denoted as a_(t) and b_(t) respectively, it is desirablefor the half-life ratio b_(t)/a_(t) to be at least 7, preferably atleast 8, more preferably at least 9, and most preferably at least 10,but not more than 20, preferably not more than 18, and most preferablynot more than 16. Even with the use of two or more organic peroxides, ata half-life ratio outside of the above range, the desired level ofrebound, compression and durability may not be achieved.

It is desirable for (a) to have a half-life a_(t) at 155° C. of at least5 seconds, preferably at least 10 seconds, and most preferably at least15 seconds, but not more than 120 seconds, preferably not more than 90seconds, and most preferably not more than 60 seconds. It is desirablefor (b) to have a half-life b_(t) at 155° C. of at least 300 seconds,preferably at least 360 seconds, and most preferably at least 420seconds, but not more than 800 seconds, preferably not more than 700seconds, and most preferably not more than 600 seconds.

Specific examples of suitable organic peroxides include dicumylperoxide, 1,1-bis(t-butylperoxy)-3,5,5-trimethylcyclohexane andα,α′-bis(t-butylperoxy)diisopropylbenzene. These organic peroxides maybe commercially available products, such as Percumil D (available fromNOF Corporation), Perhexa 3M (NOF Corporation) and Luperco 231XL(available from Atochem Co.). The use of1,1-bis(t-butylperoxy)-3,5,5-trimethylcyclohexane as above organicperoxide (a) and dicumyl peroxide as above organic peroxide (b) ispreferred.

The overall amount of organic peroxide, including (a) and (b) above, per100 parts by weight (abbreviated hereinafter as “parts”) of component A,is at least 0.1 part, preferably at least 0.2 part, more preferably atleast 0.3 part, and most preferably at least 0.4 part, but nor more that0.8 part, preferably not more than 0.7 part, more preferably not morethan 0.6 part, and most preferably not more than 0.5 part. Too littleorganic peroxide increases the time required for crosslinking,substantially lowering both productivity and compression. On the otherhand, too much organic peroxide lowers the rebound and durability of theball.

In the practice of the invention, by using in the golf ball core apolybutadiene synthesized using a rare-earth catalyst, and especially aneodymium catalyst, and by setting the amount of organic peroxide usedin the core within the above-indicated range, the golf ball of theinvention can be conferred with excellent rebound characteristics. Suchan increase in rebound allows the solid core or the golf ball as a wholeto be made correspondingly softer, resulting in desirable initialconditions on a full shot with a driver (i.e., low spin and high angleof elevation) as well as increased carry. Moreover, a soft feel onimpact can also be achieved.

The amount of organic peroxide (a) included in the solid core per 100parts of component A is preferably at least 0.05 part, more preferablyat least 0.08 part, and most preferably at least 0.1 part, butpreferably not more than 0.5 part, more preferably not more than 0.4part, and most preferably not more than 0.3 part. The amount of organicperoxide (b) included per 100 parts of component A is preferably atleast 0.05 part, more preferably at least 0.15 part, and most preferablyat least 0.2 part, but preferably not more than 0.7 part, morepreferably not more than 0.6 part, and most preferably not more than 0.5part.

Component C in the invention is an unsaturated carboxylic acid and/or ametal salt thereof. Examples of suitable unsaturated carboxylic acidsinclude acrylic acid, methacrylic acid, maleic acid and fumaric acid.Acrylic acid and methacrylic acid are especially preferred. Examples ofsuitable metal salts of the unsaturated carboxylic acids include zincsalts and magnesium salts. Of these, zinc acrylate is especiallypreferred.

The amount of component C per 100 parts of component A is generally atleast 10 parts, preferably at least 15 parts, and most preferably atleast 20 parts, but generally not more than 60 parts, preferably notmore than 50 parts, more preferably not more than 45 parts, and mostpreferably not more than 40 parts. An amount of component C outside ofthe above range may compromise the rebound characteristics and feel uponimpact of the golf ball.

Component D in the invention is an organic sulfur compound. Exemplaryorganic sulfur compounds include thiophenols, thionaphthols, halogenatedthiophenols, and metal salts thereof. Specific examples includepentachlorothiophenol, pentafluorothiophenol, pentabromothiophenol,p-chlorothiophenol, and the zinc salts thereof; diphenylpolysulfides,dlbenzylpolysulfides, dibenzoylpolysulfides, dibenzothiazoylpolysulfidesand dithiobenzoylpolysulfides having 2 to 4 sulfurs;alkylphenyldisulfides, furan ring-bearing sulfur compounds and thiophenering-bearing sulfur compounds. Diphenyldisulfide and the zinc salt ofpentachlorothiophenol are especially preferred.

The amount of component D per 100 parts of component A is generally atleast 0.1 part, preferably at least 0.2 part, more preferably at least0.4, and most preferably at least 0.7 part, but generally not more than5 parts, preferably not more than 4 parts, more preferably not more than3 parts, even more preferably not more than 2 parts, and most preferablynot more than 1.5 parts. The addition of too little component D may failto have a resilience-improving effect, whereas too much component D mayresult in a low hardness and insufficient resilience.

Component E in the invention is an inorganic filler, illustrativeexamples of which include zinc oxide, barium sulfate and calciumcarbonate. The amount of component E per 100 parts of component A isgenerally at least 5 parts, preferably at least 7 parts, more preferablyat least 10 parts, and most preferably at least 13 parts, but generallynot more than 80 parts, preferably not more than 65 parts, morepreferably not more than 50 parts, and most preferably not more than 40parts. The use of too much or too little component E may make itimpossible to achieve a golf ball having the proper weight and adesirable rebound.

If necessary, the rubber composition containing above components A to Emay include also an antioxidant. The amount of antioxidant added per 100parts of component A is generally at least 0.05 part, preferably atleast 0.1 part, and more preferably at least 0.2 part, but not more than3 parts, preferably not more than 2 parts, more preferably not more than1 part, and most preferably not more than 0.5 part.

The antioxidant may be a commercially available product, such as NocracNS-6, Nocrac NS-30 (both made by Ouchi Shinko Chemical Industry Co.,Ltd.), and Yoshinox 425 (made by Yoshitomi Pharmaceutical Industries,Ltd.).

The solid core of the inventive golf ball is produced from a rubbercomposition containing above components A to E by a process thatpreferably involves vulcanization and curing of the rubber composition.For example, vulcanization may be carried out at a temperature of 100 to200° C. for a period of 10 to 40 minutes.

The solid core formed as described above has a localized hardness whichcan be adjusted as appropriate and is not subject to any particularlimitation. That is, the core thus formed may have a localized hardnessprofile which is flat from the center to the surface of the core, orwhich varies from the center to the surface.

It is desirable for the solid core to have a diameter of at least 30 mm,preferably at least 32 mm, and most preferably at least 34 mm, but notmore than 40 mm, preferably not more than 39 mm, and most preferably notmore than 38 mm. A solid core diameter of less than 30 mm compromisesthe feel upon impact and the rebound of the golf ball. On the otherhand, at a solid core diameter of more than 40 mm, the ball has a poordurability to cracking.

The solid core has a deflection, when subjected to a load of 980 N (100kg), of at least 3.0 mm, preferably at least 3.5 mm, more preferably atleast 4.0 mm, and most preferably at least 4.3 mm, but not more than 6.0mm, preferably not more than 5.8 mm, more preferably not more than 5.5mm, and most preferably not more than 5.3 mm. A deflection of less than3.0 mm worsens the feel upon impact and, particularly on long shots suchas with a driver in which the ball incurs a large deformation, subjectsthe ball to an excessive increase in spin, reducing the carry. On theother hand, at a deflection of more than 6.0 mm, the golf ball has aless lively feel when hit and an inadequate rebound that results in apoor carry, in addition to which it has a poor durability to crackingwith repeated impact.

It is recommended that the solid core have a specific gravity (g/cm³) ofgenerally at least 0.9, preferably at least 1.0, and most preferably atleast 1.1, but not more than 1.4, preferably not more than 1.3, and mostpreferably not more than 1.2.

The thermoplastic resin composition used to form the mantle composed ofat least one layer is preferably made of 100 parts by weight of resincomponents which include a base resin of (P) an olefin/unsaturatedcarboxylic acid binary random copolymer and/or a metal ionneutralization product of an olefin/unsaturated carboxylic acid binaryrandom copolymer in admixture with (Q) an olefin/unsaturated carboxylicacid/unsaturated carboxylic acid ester ternary random copolymer and/or ametal ion neutralization product of an olefin/unsaturated carboxylicacid/unsaturated carboxylic acid ester ternary random copolymer in aweight ratio P/Q of 100:0 to 25:75, and (R) a non-ionomericthermoplastic elastomer in a weight ratio (P+Q)/R of 100:0 to 50:50; (S)5 to 80 parts by weight of a fatty acid and/or fatty acid derivativehaving a molecular weight of 280 to 1,500; and (T) 0.1 to 10 parts byweight of a basic inorganic metal compound capable of neutralizingun-neutralized acid groups in the base resin and component S.

The olefins in the above base resin, both in component P and componentQ, have a number of carbons that is generally at least 2, but not morethan 8, and preferably not more than 6. Suitable examples includeethylene, propylene, butene, pentene, hexene, heptene and octene.Ethylene is especially preferred.

Illustrative examples of the unsaturated carboxylic acid include acrylicacid, methacrylic acid, maleic acid and fumaric acid. Acrylic acid andmethacrylic acid are especially preferred.

The unsaturated carboxylic acid ester is preferably a lower alkyl esterof the unsaturated carboxylic acid. Specific examples include methylmethacrylate, ethyl methacrylate, propyl methacrylate, butylmethacrylate, methyl acrylate, ethyl acrylate, propyl acrylate and butylacrylate. Butyl acrylate (n-butyl acrylate, i-butyl acrylate) isespecially preferred.

The olefin/unsaturated carboxylic acid binary random copolymer ofcomponent P and the olefin/unsaturated carboxylic acid/unsaturatedcarboxylic acid ester ternary random copolymer of component Q (thecopolymers in components P and Q are hereinafter referred tocollectively as “random copolymers”) can each be obtained by suitablyformulating the above-described materials and using a known method tocarry out random copolymerization.

It is recommended that the above random copolymers be prepared such asto have a specific unsaturated carboxylic acid content (sometimesreferred to hereinafter as the “acid content”). The amount ofunsaturated carboxylic acid included within the random copolymer ofcomponent P is generally at least 4 wt %, preferably at least 6 wt %,more preferably at least 8 wt %, and most preferably at least 10 wt %,but generally not more than 30 wt %, preferably not more than 20 wt %,more preferably not more than 18 wt %, and most preferably not more than15 wt %.

Similarly, it is recommended that the amount of unsaturated carboxylicacid included within the random copolymer of component Q be generally atleast 4 wt %, preferably at least 6 wt %, and most preferably at least 8wt %, but not more than 15 wt %, preferably not more than 12 wt %, andmost preferably not more than 10 wt %. If the random copolymers have toolow an acid content, the resilience may decline. On the other hand, toohigh an acid content may lower the processability of the thermoplasticresin composition.

The metal ion neutralization product of an olefin/unsaturated carboxylicacid binary random copolymer in component P and the metal ionneutralization product of an olefin/unsaturated carboxylicacid/unsaturated carboxylic acid ester ternary random copolymer incomponent Q (the metal ion neutralization products of copolymers incomponents P and Q are hereinafter referred to collectively as “metalion-neutralized random copolymers”) can be obtained by partiallyneutralizing the acid groups on the random copolymer with metal ions.

Illustrative examples of metal ions for neutralizing the acid groupsinclude Na⁺, K⁺, Li⁺, Zn²⁺, Cu²⁺, Mg²⁺, Ca²⁺, Co²⁺, Ni²⁺ and Pb²⁺.Preferred metal ions include Na⁺, Li⁺, Zn²⁺ and Mg²⁺. The use of Zn²⁺ isespecially recommended.

In the practice of the invention, the metal ion-neutralized randomcopolymers may be prepared by neutralization with the above metal ions.For example, use may be made of a neutralization method that involvesthe use of compounds such as the formates, acetates, nitrates,carbonates, bicarbonates, oxides, hydroxides or alkoxides of the abovemetal ions. The degree of neutralization of the random copolymer bythese metal ions is not subject to any particular limitation.

In the invention, the metal ion-neutralized random copolymers arepreferably zinc ion-neutralized ionomer resins. Such ionomer resinsincrease the melt flow rate of the material, facilitate adjustment tothe subsequently described optimal melt flow rate, and thus enable themoldability of the thermoplastic resin composition to be improved.

Commercial products may be used in the base resin made up of abovecomponents P and Q. Examples of commercial products that may be used asthe random copolymer in component P include Nucrel 1560, Nucrel 1214 andNucrel 1035 (all products of DuPont-Mitsui Polychemicals Co., Ltd.); andEscor 5200, Escor 5100 and Escor 5000 (all products of ExxonMobilChemical). Examples of commercial products that may be used as therandom copolymer in component Q include Nucrel AN4311 and Nucrel AN4318(both products of DuPont-Mitsui Polychemicals Co., Ltd.); and EscorATX325, Escor ATX320 and Escor ATX310 (all products of ExxonMobilChemical).

Examples of commercial products that may be used as the metalion-neutralized random copolymer in component P include Himilan 1554,Himilan 1557, Himilan 1601, Himilan 1605, Himilan 1706 and HimilanAM7311 (all products of DuPont-Mitsui Polychemicals Co., Ltd.), Surlyn7930 (produced by E.I. du Pont de Nemours and Co., Inc.) and Iotek 3110and Iotek 4200 (both products of ExxonMobil Chemical). Examples ofcommercial products that may be used as the metal ion-neutralized randomcopolymer in component Q include Himilan 1855, Himilan 1856 and HimilanAM7316 (all products of DuPont-Mitsui Polychemicals Co., Ltd.), Surlyn6320, Surlyn 8320, Surlyn 9320 and Surlyn 8120 (all products of E.I. duPont de Nemours and Co., Inc.), and Iotek 7510 and Iotek 7520 (bothproducts of ExxonMobil Chemical). Examples of zinc-neutralized ionomerresins that can be preferably used as the above metal ion-neutralizedrandom copolymers include Himilan 1706, Himilan 1557 and Himilan AM7316.

When the above-described base resin is prepared, the weight ratio P/Q ofcomponent P to component Q must be set at from 100:0 to 25:75,preferably from 100:0 to 50:50, more preferably from 100:0 to 75:25, andmost preferably 100:0. Too little component P lowers the resilience ofthe molded material.

In addition, by adjusting the relative proportions of random copolymerand metal ion-neutralized random copolymer metal in the base resin ofabove components P and Q, the moldability of the thermoplastic resincomposition can be further improved. It is recommended that that theratio of random copolymer to metal ion-neutralized random copolymer begenerally from 0:100 to 60:40, preferably from 0:100 to 40:60, morepreferably from 0:100 to 20:80, and most preferably 0:100. The presenceof too much random copolymer may lower the processability during mixing.

Component R is a non-ionomeric thermoplastic elastomer which isoptionally included to further enhance both the feel of the golf ballupon impact and its rebound characteristics. In the invention, theabove-described base resin and component R are referred to collectivelyas the “resin components”. Specific examples of non-ionomericthermoplastic elastomers that may be used as component R include olefinelastomers, styrene elastomers, polyester elastomers, urethaneelastomers and polyamide elastomers. The use of olefin elastomers andpolyester elastomers is preferred for further increasing resilience.

Examples of commercial products that may be used as component R includeolefin elastomers such as Dynaron (manufactured by JSR Corporation) andpolyester elastomers such as Hytrel (manufactured by DuPont-Toray Co.,Ltd.).

It is recommended that the amount of component R per 100 parts of thebase resin in the thermoplastic resin composition be at least 0 part,preferably at least 1 part, more preferably at least 2 parts, even morepreferably at least 3 parts, and most preferably at least 4 parts, butnot more than 100 parts, preferably not more than 60 parts, morepreferably not more than 40 parts, and most preferably not more than 20parts. Too much component R may lower the compatibility of the mixtureand markedly compromise the durability of the golf ball.

Next, component S in the thermoplastic resin composition is a fatty acidor fatty acid derivative having a molecular weight of 280 to 1,500. Thiscomponent has a very low molecular weight compared to the base resin andis used to adjust the melt viscosity of the mixture to a suitable level,particularly to help improve flow. Component S has a relatively highcontent of acid groups (or derivatives thereof) and can suppress anexcessive loss of resilience.

The molecular weight of the fatty acid or fatty acid derivative ofcomponent S is at least 280, preferably at least 300, more preferably atleast 330, and most preferably at least 360, but not more than 1,500,preferably not more than 1,000, more preferably not more than 600, andmost preferably not more than 500. Too low a molecular weight mayprevent a better heat resistance from being achieved, whereas too high amolecular weight may make it impossible to improve flow.

Preferred examples of the fatty acid or fatty acid derivative serving ascomponent S include unsaturated fatty acids having a double bond ortriple bond on the alkyl group and derivatives thereof, and saturatedfatty acids in which all the bonds on the alkyl group are single bondsand derivatives thereof. It is recommended that the number of carbons onthe molecule be generally at least 18, preferably at least 20, morepreferably at least 22, and most preferably at least 24, but not morethan 80, preferably not more than 60, more preferably not more than 40,and most preferably not more than 30. Too few carbons may prevent abetter heat resistance from being achieved and may also make the contentof acid groups so high as to diminish the flow-enhancing effect onaccount of interactions between acid groups in component S and acidgroups present in the base resin. On the other hand, too many carbonsincreases the molecular weight, which may prevent the flow-enhancingeffect from being achieved.

Specific examples of fatty acids that may be used as component S includestearic acid, 12-hydroxystearic acid, behenic acid, oleic acid, linoleicacid, linolenic acid, arachidic acid and lignoceric acid. Of these,stearic acid, arachidic acid, behenic acid and lignoceric acid arepreferred. Behenic acid is especially preferred.

Fatty acid derivatives which may be used as component S include metallicsoaps in which the proton on the acid group of the fatty acid has beensubstituted with a metal ion. Metal ions that may be used in suchmetallic soaps include Na⁺, Li⁺, Ca²⁺, Mg²⁺, Zn²⁺, Mn²⁺, Al³⁺, Ni²⁺,Fe²⁺, Fe³⁺, Cu²⁺, Sn²⁺, Pb²⁺ and Co²⁺. Of these, Ca²⁺, Mg²⁺ and Zn²⁺ arepreferred.

Specific examples of fatty acid derivatives that may be used ascomponent S include magnesium stearate, calcium stearate, zinc stearate,magnesium 12-hydroxystearate, calcium 12-hydroxystearate, zinc12-hydroxystearate, magnesium arachidate, calcium arachidate, zincarachidate, magnesium behenate, calcium behenate, zinc behenate,magnesium lignocerate, calcium lignocerate and zinc lignocerate. Ofthese, magnesium stearate, calcium stearate, zinc stearate, magnesiumarachidate, calcium arachidate, zinc arachidate, magnesium behenate,calcium behenate, zinc behenate, magnesium lignocerate, calciumlignocerate and zinc lignocerate are preferred.

Moreover, known metallic soap-modified ionomers, including thosedescribed in U.S. Pat. Nos. 5,312,857, 5,306,760 and InternationalApplication WO 98/46671, may be used as the base resin (above componentsP and Q) in combination with above component S.

Component T is a basic inorganic metal compound which can neutralizeacid groups in the base resin and component S. When a metallicsoap-modified ionomer resin (e.g., the metallic soap-modified ionomerresins mentioned in the above-cited prior-art patent publications) isused alone without including component T, the metallic soap and theun-neutralized acid groups present on the ionomer resin undergo exchangereactions during mixture under heating, generating a large amount offatty acid. Because the fatty acid has a low thermal stability andreadily vaporizes during molding, it may cause molding defects.Moreover, it adheres to the surface of the molded article, which cansubstantially lower paint film adhesion.

To overcome such problems and improve the resilience of the moldedmantle, it is essential to include a basic inorganic metal compound(component T) which neutralizes acid groups present in the base resinand in component S.

That is, incorporating above component T in the thermoplastic resincomposition results in a suitable degree of neutralization of the acidgroups in the base resin and in component S. Moreover, optimizing thevarious components in this way produces synergistic effects whichincrease the thermal stability of the mixture, impart a goodprocessability and make it possible to enhance the resilience of themantle.

It is recommended that the basic inorganic metal compound used ascomponent T be one which has a high reactivity with the base resin andincludes no organic acids in the reaction by-products, thus enabling thedegree of neutralization of the mixture to be increased without a lossof thermal stability.

Illustrative examples of the metal ions in the basic inorganic metalcompound serving as component T include Li⁺, Na⁺, K⁺, Ca²⁺, Mg²⁺, Zn²⁺,Al³⁺, Ni²⁺, Fe²⁺, Fe³⁺, Cu²⁺, Mn²⁺, Sn²⁺, Pb²⁺ and Co²⁺. Known basicinorganic fillers containing these metal ions may be used as the basicinorganic metal compound. Specific examples include magnesium oxide,magnesium hydroxide, magnesium carbonate, zinc oxide, sodium hydroxide,sodium carbonate, calcium oxide, calcium hydroxide, lithium hydroxideand lithium carbonate. A hydroxide or a monoxide is recommended. Calciumhydroxide and magnesium oxide, both of which have a high reactivity withthe base resin, are preferred. Calcium hydroxide is especiallypreferred.

In the golf ball of the invention, the above-described thermoplasticresin composition which makes up the mantle having at least one layer isarrived at by blending specific respective amounts of components S and Twith the resin components; that is, the base resin containing specificrespective amounts of components P and Q, and optional component R. Sucha thermoplastic resin composition has excellent thermal stability, flowproperties and moldability, and can confer the molded article with amarkedly improved resilience.

Components S and T are compounded in respective amounts, per 100 partsby weight of the resin components suitably formulated from components P,Q and R, of at least 5 parts by weight, preferably at least 10 parts byweight, more preferably at least 15 parts by weight, and most preferablyat least 18 parts by weight, but not more than 80 parts by weight,preferably not more than 40 parts by weight, more preferably not morethan 25 parts by weight, and most preferably not more than 22 parts byweight, of component S; and at least 0.1 part by weight, preferably atleast 0.5 part by weight, more preferably at least 1 part by weight, andmost preferably at least 2 parts by weight, but not more than 10 partsby weight, preferably not more than 8 parts by weight, more preferablynot more than 6 parts by weight, and most preferably not more than 5parts by weight, of component T. Too little component S lowers the meltviscosity, resulting in inferior processability, whereas too much lowersthe durability. Too little component T fails to improve thermalstability and resilience, whereas too much instead lowers the heatresistance of the thermoplastic resin composition due to the presence ofexcess basic inorganic metal compound.

In the thermoplastic resin composition which is used to form the mantlehaving one or more layer in the inventive golf ball and is formulatedfrom the respective above-indicated amounts of the foregoing resincomponents and components S and T, it is recommended that at least 50mol %, preferably at least 60 mol %, more preferably at least 70 mol %,and most preferably at least 80 mol %, of the acid groups beneutralized. A high degree of neutralization such as this makes itpossible to more reliably suppress the exchange reactions that become aproblem when only a base resin and a fatty acid or fatty acid derivativeare used as in the above-cited prior art, thus preventing the formationof fatty acid. As a result, there is obtained a material of greatlyincreased thermal stability and good processability which can provide amantle of much better resilience than prior-art ionomer resins.

Degree of neutralization, as used above, refers to the degree ofneutralization of acid groups present within the mixture of the baseresin and the fatty acid or fatty acid derivative serving as componentS, and differs from the degree of neutralization of the ionomer resinitself when an ionomer resin is used as the metal ion-neutralized randomcopolymer in the base resin. A mixture according to the invention havinga certain degree of neutralization, when compared with an ionomer resinby itself having the same degree of neutralization, contains a verylarge number of metal ions. This large number of metal ions increasesthe density of ionic crosslinks that contribute to improved reactivity,making it possible to confer the molded article with excellentresilience.

To more reliably achieve both a high degree of neutralization and goodflow characteristics, it is recommended that the acid groups in theabove-described mixture be neutralized with transition metal ions andalkali metal and/or alkaline earth metal ions. Although transition metalions have a weaker ionic cohesion than alkali metal and alkaline earthmetal ions, the combined use of these different types of ions toneutralize acid groups in the mixture can provide a substantialimprovement in the flow properties of the thermoplastic resincomposition.

The molar ratio between the transition metal ions and the alkali metaland/or alkaline earth metal ions may be adjusted as appropriate. It isrecommended that the ratio be within a range of generally 10:90 to90:10, preferably 20:80 to 80:20, more preferably 30:70 to 70:30, andmost preferably 40:60 to 60:40. Too low a molar ratio of transitionmetal ions may fail to provide sufficient improvement in the flowcharacteristics of the thermoplastic resin composition. On the otherhand, too high a molar ratio may lower the resilience of the mantlemolded from the composition.

Specific, non-limiting, examples of the metal ions include zinc ions asthe transition metal ions and at least one type of ion selected fromamong sodium, lithium and magnesium ions as the alkali metal or alkalineearth metal ions.

A known method may be used to obtain a mixture in which the desiredamount of acid groups have been neutralized with transition metal ionsand alkali metal or alkaline earth metal ions. Specific examples ofmethods of neutralization with transition metal ions, particularly zincions, include the use of zinc soaps as the fatty acid derivative, theuse of zinc-neutralized products (e.g., zinc ion-neutralized ionomerresins) when formulating component P and component Q as the base resin,and the use of zinc compounds such as zinc oxide as the basic inorganicmetal compound of component T.

In the golf ball of the invention, the above-described thermoplasticresin composition from which the mantle having at least one layer ismade may include also suitable amounts of any additives that may berequired for the intended use of the material. For example, if thematerial is to be used as a cover stock, such additives as pigments,dispersants, antioxidants, ultraviolet absorbers and light stabilizersmay be added to the essential ingredients described above. When suchadditives are included in the composition, they may be incorporated inan amount, per 100 parts by weight of the essential ingredients of thecomposition (the resin components and components S and T), of preferablyat least 0.1 part by weight, more preferably at least 0.5 part byweight, and most preferably at least 1 part by weight, but not more than10 parts by weight, preferably not more than 6 parts by weight, and mostpreferably not more than 4 parts by weight.

The thermoplastic resin composition may be obtained by preparing amixture of the above-described essential ingredients and whateveroptional ingredients may be needed, then heating and working togetherthe mixture under suitable conditions, such as a heating temperature of150 to 250° C. and using an internal mixer such as a kneading-typetwin-screw extruder, a Banbury mixer or a kneader. Any suitable methodmay be used without particular limitation to blend various additiveswith the above-described essential ingredients of the invention. Forexample, the additives may be combined with the essential ingredients,and heating and mixture of all the ingredients carried out at the sametime. Alternatively, the essential ingredients may first be heated andmixed, following which the optional additives may be added and theoverall composition subjected to additional heating and mixture.

The thermoplastic resin composition should have a melt flow rateadjusted to ensure flow characteristics that are particularly suitablefor injection molding and thus improve moldability. Specifically, it isrecommended that the melt flow rate, as measured according to JIS-K7210at a temperature of 190° C. and under a load of 21.18 N (2.16 kgf), beset to generally at least 0.5 dg/min, preferably at least 1 dg/min, morepreferably at least 1.5 dg/min, and even more preferably at least 2dg/min, but generally not more than 20 dg/min, preferably not more than10 dg/min, more preferably not more than 5 dg/min, and most preferablynot more than 3 dg/min. Too large or small a melt flow rate may resultin a marked decline in melt processability.

The above thermoplastic resin composition is preferably characterizedalso in terms of the relative absorbance in infrared absorptionspectroscopy, representing the ratio of absorbance at the absorptionpeak attributable to carboxylate anion stretching vibrations normallydetected at 1530 to 1630 cm⁻¹ to the absorbance at the absorption peakattributable to carbonyl stretching vibrations normally detected at 1690to 1710 cm⁻¹. For the sake of clarity, this ratio may be expressed asfollows: (absorbance of absorption peak for carboxylate anion stretchingvibrations)/(absorbance of absorption peak for carbonyl stretchingvibrations).

Here, “carboxylate anion stretching vibrations” refers to vibrations bycarboxyl groups from which the proton has dissociated (metalion-neutralized carboxyl groups), whereas “carbonyl stretchingvibrations” refers to vibrations by undissociated carboxyl groups. Theratio between these respective peak intensities depends on the degree ofneutralization. In the ionomer resins having a degree of neutralizationof about 50 mol % which are commonly used, the ratio, between these peakabsorbances is about 1:1.

To improve the thermal stability, flow, processability and resilience ofthe thermoplastic resin composition used in the invention, it isrecommended that the composition have a carboxylate anion stretchingvibration peak absorbance which is at least 1.3 times, preferably atleast 1.5 times, and most preferably at least 2 times, the carbonylstretching vibration peak absorbance. The absence of any carbonylstretching vibration peak is especially preferred.

The thermal stability of the thermoplastic resin composition can bemeasured by thermogravimetry. It is recommended that, inthermogravimetry, the composition have a weight loss at 250° C., basedon the weight of the composition at 25° C., of generally not more than 2wt %, preferably not more than 1.5 wt %, and most preferably not morethan 1 wt %.

A known method may be used to form a mantle of at least one layer fromthe above-described thermoplastic resin composition. The method is notsubject to any particular limitation and may be, for example, a processin which a prefabricated core is placed within a mold, and thethermoplastic resin composition, after being heated, mixed and melted,is injection molded about the core. Such a process is highly desirablebecause it allows production of the golf ball to be carried out in astate where excellent flow properties and moldability are assured.Moreover, the resulting golf ball has a high rebound.

Alternatively, a method may be employed in which the thermoplastic resincomposition serving as the mantle-forming material is pre-molded into apair of hemispherical half-cups, following which the half-cups areplaced around the core and molded under applied pressure at 120 to 170°C. for a period of 1 to 5 minutes.

The mantle composed of at least one layer has a thickness per layer ofat least 0.5 mm, and preferably at least 0.7 mm, but not more than 2.0mm, and preferably not more than 1.8 mm. At a thickness per mantle layerof less than 0.5 mm, the presence of a mantle has substantially noeffect. On the other hand, a thickness per layer of more than 2.0 mmcompromises the feel on impact and the rebound of the ball.

In the mantle having at least one layer, the mantle layer in contactwith the cover (outermost layer of the mantle) has a Shore D hardness ofat least 20, and preferably at least 25, but not more than 60, andpreferably not more than 58. At a Shore D hardness in the outermostlayer of the mantle of less than 20, the rebound of the ball decreases.On the other hand, at a Shore D hardness of more than 60, the feel ofthe golf ball at the time of impact is greatly diminished.

It is critical that the Shore D hardness of the outermost layer of themantle in the inventive golf ball be no greater than the subsequentlydescribed Shore D hardness of the cover. This relationship between theShore D hardness of the outermost layer of the mantle and the shore Dhardness of the cover enables a lower spin and a higher angle ofelevation to be achieved in the golf ball. Moreover, when an ionomerresin having a high degree of neutralization is used as themantle-forming material, a high rebound is also achieved. These effectswork together to provide a good carry.

Preferably the mantle consists of an inner layer and an outer layer.

The inventive golf ball has a cover made primarily of a mixturecontaining (M) an amino-terminated block polymer and (N) an ionomerresin, in a weight ratio M/N of 3/97 to 60/40. This mixture is sometimesreferred to hereinafter as the “cover stock”.

The amino-terminated block polymer (M) is preferably a crystallineolefin block-bearing block copolymer whose ends have been modified withamino groups.

The crystalline olefin block-bearing block copolymer is preferably onehaving hard segments composed of crystalline olefin blocks (Co) orcrystalline olefin blocks (Co) in combination with crystalline styreneblocks (Cs), and having soft segments composed of blocks of ethylene andbutylene with a relatively random copolymeric structure (EB). The use ofa block copolymer having a molecular structure with a hard segment atone or both ends, that is, a Co-EB, Co-EB-Co or Cs-EB-Co structure, ispreferred. Illustrative examples of the crystalline olefin blocksinclude crystalline polyethylene blocks and crystalline polypropyleneblocks. Crystalline polyethylene blocks are especially preferred.

These block copolymers having crystalline olefin blocks can be preparedby the hydrogenation of a polybutadiene or a styrene-butadienecopolymer.

The polybutadiene or styrene-butadiene copolymer used in hydrogenationis preferably a polybutadiene in which the butadiene structure contains1,4 polymer blocks which are at least 95 wt % composed of 1,4 units, andthe overall butadiene structure has a 1,4 unit content of at least 50 wt%, and preferably at least 80 wt %.

It is especially preferable for the above-described block copolymerhaving a Co-EB-Co structure to be prepared by the hydrogenation of apolybutadiene in which both ends of the molecular chain are 1,4polymerization products rich in 1,4 units, and the center portion ofwhich contains a mixture of 1,4 units and 1,2 units.

In cases where the ends of the crystalline olefin block-bearing blockcopolymer are modified with amino groups, the modification of styreneblock ends with amino groups is preferred.

The degree of hydrogenation in the polybutadiene or styrene-butadienecopolymer hydrogenation product, expressed as the percent of doublebonds in the polybutadiene or styrene-butadiene copolymer that areconverted to saturated bonds, is preferably 60 to 100%, and mostpreferably 90 to 100%. Too low a degree of hydrogenation may lead todeterioration such as gelation when blended with the ionomer resin andother components. Moreover, the cover in the completed golf ball mayhave a poor weather resistance and a poor durability to impact.

In the above block copolymers having crystalline olefin blocks, the hardsegment content is preferably 10 to 50 wt %. A hard segment contentwhich is too high may result in a poor flexibility that keeps theobjects of the invention from being effectively achieved, whereas a hardsegment content which is too low may compromise the moldability of theblend.

This crystalline olefin block-bearing block copolymer has anumber-average molecular weight of preferably 30,000 to 800,000.

The above-described block copolymer has a melt index at 230° C. ofpreferably 0.5 to 15 g/10 min, and most preferably 1 to 7 g/10 min.Outside of this range, problems such as weld lines, sink marks and shortshots may arise during injection molding.

The ionomer resin (N) used in the invention includes any ionomer resinsthat have hitherto been employed in cover stocks for golf balls.Preferably, the ionomer resin (N) is one containing both:

(N-1) an olefin/unsaturated carboxylic acid binary random copolymerand/or a metal ion neutralization product of an olefin/unsaturatedcarboxylic acid binary random copolymer, and

(N-2) an olefin/unsaturated carboxylic acid/unsaturated carboxylic acidester ternary random copolymer and/or a metal ion neutralization productof an olefin/unsaturated carboxylic acid/unsaturated carboxylic acidester ternary random copolymer.

α-Olefins may be suitably used as the olefins in components N-1 and N-2.Specific examples of suitable α-olefins include ethylene, propylene and1-butene. Of these, ethylene is especially preferred. A plurality ofthese olefins may be used in combination.

α,β-Unsaturated carboxylic acids having 3 to 8 carbons may be suitablyused as the unsaturated carboxylic acids in components N-1 and N-2.Specific examples of suitable α,β-unsaturated carboxylic acids having 3to 8 carbons include acrylic acid, methacrylic acid, ethacrylic acid,itaconic acid, maleic acid and fumaric acid. Of these, acrylic acid andmethacrylic acid are preferred. A plurality of these unsaturatedcarboxylic acids may be used in combination.

Lower alkyl esters of the above unsaturated carboxylic acids aresuitable as the unsaturated carboxylic acid ester in component N-2.Examples includes those obtained by reacting a lower alcohol such asmethanol, ethanol, propanol, n-butanol or isobutanol with the aboveunsaturated carboxylic acids. Acrylic acid esters and methacrylic acidesters are especially preferred.

Suitable examples of the unsaturated carboxylic acid ester in componentN-2 include methyl methacrylate, ethyl methacrylate, propylmethacrylate, butyl methacrylate, methyl acrylate, ethyl acrylate,propyl acrylate and butyl acrylate. Butyl acrylate (n-butyl acrylate,i-butyl acrylate) is especially preferred. A plurality of theseunsaturated carboxylic acid esters may be used in combination.

When the above olefin/unsaturated carboxylic acid copolymer orolefin/unsaturated carboxylic acid/unsaturated carboxylic acid estercopolymer is prepared, other monomers may optionally be copolymerizedtherewith, provided this does not compromise the objects of theinvention.

The content of unsaturated carboxylic acid within these copolymers ispreferably 5 to 20 wt % in component N-1 and preferably 1 to 10 wt % incomponent N-2. If the unsaturated carboxylic acid content is too low,the rigidity and resilience of the cover become small, which may lowerthe flight characteristics of the golf ball. On the other hand, acontent of unsaturated carboxylic acid which is too high may result in acover of inadequate flexibility.

The content of unsaturated carboxylic acid ester in component N-2 ispreferably 12 to 45 wt %. If the unsaturated carboxylic acid estercontent is too low, a softening effect may not be achieved, whereas ifit is too high, the resilience of the cover may decrease.

When above components N-1 and N-2 are blended together, it is desirablefor them to be used in a weight ratio (N-1)/(N-2) of preferably 100/0 to25/75, and most preferably 100/0 to 50/50. The addition of too muchcomponent N-2 may result in an inadequate resilience.

The ionomer resin N used in the invention is preferably one obtained byneutralizing the above-described copolymers with metal ions having avalence of 1 to 3. Examples of metal ions with a valence of 1 to 3 thatare suitable for neutralization include Na⁺, K⁺, Li⁺, Mg²⁺, Ca²⁺, Zn²⁺,Al³⁺, Fe²⁺ and Fe³⁺.

Such metal ions can be introduced by reacting the above-describedcopolymer with, for example, a hydroxide, methoxide, ethoxide,carbonate, nitrate, formate, acetate or oxide of the above metal havinga valence of 1 to 3.

It is advantageous for the degree of neutralization of the carboxylicacid included within the above-described copolymer to be such that atleast 10 mol %, preferably at least 30 mol %, and up to 100 mol %,preferably up to 90 mol %, of the carboxylic acid groups on thecopolymer are neutralized with metal ions. A low degree ofneutralization may result in a low resilience.

To improve resilience, it is desirable for a monovalent metal ionomerand a divalent metal ionomer to be mixed and used together, preferablysuch that the weight ratio of the monovalent metal ionomer to thedivalent metal ionomer is from 20/80 to 80/20.

It is known that blending together suitable amounts of ionomer resinscontaining different monovalent, divalent or trivalent metal ionsenables a balance to be achieved between the resilience and durabilityof a layer composed primarily of ionomer resin. Blending in this way isdesirable in the present invention as well.

The ionomer resin N used in the invention may be a commercial product,illustrative examples of which include Surlyn (produced by E.I. DuPontde Nemours and Company) and Himilan (produced by DuPont-MitsuiPolychemicals Co., Ltd.).

In the practice of the invention, the amino-terminated block polymer (M)and the ionomer resin (N) are blended in proportions, based on acombined amount of 100 parts by weight, of 3 to 60 parts by weight,preferably 10 to 60 parts by weight, and most preferably 20 to 45 partsby weight, of component M; and 40 to 97 parts by weight, preferably 40to 90 parts by weight, and most preferably 55 to 80 parts by weight ofcomponent N. The inclusion of too little component M fails to provideadequate softening of the ionomer resin, as a result of which sufficientimprovement in the feel and controllability of the ball are notachieved. On the other hand, too much component M compromises the cutresistance of the cover.

If necessary, the cover stock used in the invention may have addedthereto various additives, such as pigments, dispersants, antioxidants,ultraviolet absorbers, light stabilizers and inorganic fillers, insofaras the objects of the invention are achievable.

Specific examples of such additives include zinc oxide, barium sulfate,titanium dioxide, magnesium oxide, magnesium hydroxide, magnesiumcarbonate, sodium hydroxide, sodium carbonate, calcium oxide, calciumhydroxide, lithium hydroxide, lithium carbonate and magnesium stearate.

The amount of such additives included in the cover stock, per 100 partsby weight of the mixture of components M and N, is generally 0.1 to 50parts by weight, preferably 0.5 to 30 parts by weight, and morepreferably 1 to 6 parts by weight. The use of too much additive maylower the durability of the cover, whereas the use of too little mayfail to achieve the desired effects of those additives.

The cover obtained from the above-described cover stock has a Shore Dhardness of at least 50, and preferably at least 53, but not more than70, and preferably not more than 64. A Shore D hardness which is too lowcompromises the rebound of the ball, whereas a Shore D hardness which istoo high fails to provide an improved feel and controllability. “Shore Dhardness,” as used herein, refers to the hardness measured with a type Ddurometer as described in ASTM D2240.

The method of preparing the above-described cover stock is not subjectto any particular limitation. For example, the cover stock may beobtained by working together the above components under applied heat at150 to 250° C. using an internal mixer such as a kneading-typetwin-screw extruder, a Banbury mixer or a kneader.

When various additives are included in the cover stock together withabove components M and N, any suitable method of incorporation may beused. That is, the additives may be blended together with components Mand N, and heated and mixed at the same time. Alternatively, componentsM and N may first be heated and mixed, then the desired additives added,followed by further heating and mixing.

The above-described cover stock provides a cover of excellentresilience.

Combining the soft core and the cover described above enables thehardness of the golf ball to be lowered without sacrificing carry, thusachieving a soft feel upon impact. Moreover, because the golf ball has alower hardness, the contact surface area between the club and the golfball at the time of impact increases, dispersing the force of impactwhen the ball is hit and thus further enhancing the scuff resistance ofthe ball.

The multi-piece solid golf balls of the invention are composed of theabove-described core, a mantle of at least one layer which is made ofthe above-described thermoplastic resin composition and encloses thecore, and a cover which is made of the above-described cover stock andencloses the mantle.

As with the formation of the mantle, the method used to form the covermay be one known to the art and is not subject to any particularlimitation. For example, use may be made of a method in which amantle-covered core is placed within a mold and the cover stock, afterbeing heated, mixed and melted, is injection molded about themantle-covered core. Such a process is desirable both because it allowsproduction of the golf ball to be carried out in a state where excellentflow properties and moldability are assured, and because the resultinggolf ball has a high rebound.

Alternatively, a method may be employed in which the cover stock of theinvention is pre-molded into a pair of hemispherical half-cups,following which the half-cups are placed around the mantle-covered coreand molded under applied pressure at 120 to 170° C. for a period of 1 to5 minutes.

To ensure flow characteristics which are particularly suitable forinjection molding and to improve the moldability, it is desirable toadjust the melt flow rate of the above-described cover stock.Specifically, it is recommended that the melt flow rate, as measured inaccordance with JIS-K6760 at a temperature of 190° C. and under a loadof 21.18 N (2.16 kgf), be generally at least 0.5 dg/min, preferably atleast 1 dg/min, more preferably at least 1.5 dg/min, and most preferablyat least 2.0 dg/min, but generally not more than 20 dg/min, preferablynot more than 10 dg/min, more preferably not more than 5 dg/min, andmost preferably not more than 3 dg/min. If the cover stock has too largeor too small a melt flow rate, the melt processability may decreasemarkedly.

The cover formed from the cover stock has a thickness of at least 0.5mm, preferably at least 0.9 mm, and most preferably at least 1.1 mm, butnot more than 2.5 mm and preferably not more than 2.0 mm. A cover whichis too thick has a diminished resilience, whereas one that is too thinhas a poor durability.

In the multi-piece solid golf ball of the invention, it is desirable forthe surface of the cover to have numerous dimples formed thereon, andfor the cover to be administered various treatment such as surfacepreparation, stamping and painting. The arrangement of the dimples ispreferably such that a great circle which intersects no dimples cannotbe traced on the surface of the golf ball. The existence of even onegreat circle which does not intersect any dimples may give rise tovariability in the flight of the ball.

It is preferable for the number of dimple types and the total number ofdimples to be optimized. Synergistic effects arising from optimizationof the number of dimple types and the total number of dimples enables agolf ball to be achieved which has a more stable trajectory and a betteroverall flight performance, including carry.

The number of dimple types refers herein to the number of types ofdimples of mutually differing diameter and/or depth. It is recommendedthat this number of dimple types be generally at least two, andpreferably at least three, but not more than eight, and preferably notmore than six.

It is also recommended that the total number of dimples on the surfaceof the golf ball be generally at least 300, and preferably at least 320,but not more than 480, and preferably not more than 455. A total numberof dimples that is too low or too high may prevent the optimal amount oflift from being achieved, resulting in a shorter carry.

It is recommended that the golf ball of the invention have an optimizeddimple volume occupancy VR and an optimized dimple surface coverage SR,both of which are expressed in percent. These parameters VR and SR, whenboth optimized, act synergistically to improve the trajectory of theball and increase its carry, and also help the ball achieve a properbalance between lift and drag, thus making it possible to provide abetter overall flight performance.

The dimple volume occupancy VR is defined as the ratio of the sum of thevolumes of individual dimples on the surface of the golf ball to thevolume of a hypothetical sphere represented by the surface of the golfball were it to have no dimples, and is expressed in percent. Themulti-piece solid golf ball of the invention has a VR value of generallyat least 0.70%, and preferably at least 0.75%, but generally not morethan 1.00%, preferably not more than 0.82%, and most preferably not morethan 0.79%.

The dimple surface coverage SR is defined as the ratio of the sum of thesurface areas of individual dimples, each dimple surface area beingcircumscribed by an edge of the dimple, to the surface area of the samehypothetical sphere as described above, and is likewise expressed inpercent. The inventive golf ball has an SR value of generally at least70%, and preferably at least 72%, but generally not more than 85%, andpreferably not more than 83%.

A VR value or SR value outside of the above respective ranges mayprevent an optimal trajectory from being achieved and thus lower thecarry of the ball.

The combination of the above-described solid core and cover with theforegoing relatively high-trajectory dimples helps prevent the ball fromdropping at too steep an angle and enables the carry of the ball to beextended in a higher and flatter trajectory.

The above-described dimple volume occupancy VR and dimple surfacecoverage SR are values obtained from measurements of dimples on a fullymanufactured golf ball. For example, when the surface of the ball issubjected to finishing treatment (e.g., painting, stamping) after thecover has been formed, VR and SR are calculated based on the shape ofthe dimples on the manufactured ball once all such treatment has beencompleted.

The multi-piece solid golf ball of the invention can be manufactured inaccordance with the Rules of Golf for use in competitive play, in whichcase the ball may be formed to a diameter of not less than 42.67 mm anda weight of not more than 45.93 g, and preferably 45.0 to 45.93 g.

The multi-piece solid golf ball of the invention, which is constructedof the above-described core, mantle and cover and which preferably bearsnumerous dimples on the surface of the cover thereon, has a deflectionwhen subjected to a load of 980 N (100 kgf) of at least 3.0 mm,preferably at least 3.2 mm, more preferably at least 3.4 mm, and mostpreferably at least 3.6 mm, but not more than 5.0 mm, preferably notmore than 4.8 mm, more preferably not more than 4.6 mm, and mostpreferably not more than 4.4 mm. At a deflection of less than 3.0 mm,the feel upon impact is poor. Moreover, particularly on long shots witha driver or the like in which the ball undergoes large deformation, theball takes on too much spin and fails to travel as far. On the otherhand, at a deflection of more than 5.0 mm, the ball has a less livelyfeel and does not exhibit sufficient rebound, resulting in a shortercarry. Moreover, it has a poor durability to cracking with repeatedimpact.

EXAMPLES

The following examples and comparative examples are given by way ofillustration and not by way of limitation.

Examples 1 to 3, Comparative Examples 1 to 3

Solid cores were produced by using the rubber compositions shown inTable 1 and vulcanizing at 155° C. for 17 minutes.

In each example, a mantle-forming material of the composition shown inTable 2 was mixed in a kneading-type twin-screw extruder at 200° C. toform the mantle material in pelletized form. This material was theninjected into a mold in which the above solid core had been placed,thereby producing a mantle-covered solid core.

A material of the composition shown in Table 3 was mixed at 200° C. in akneading-type twin-screw extruder to form a cover stock in pelletizedform. The cover stock was then injected into a mold in which the abovemantle-covered solid core had been placed, thereby producing amulti-piece solid golf ball.

Details concerning the combination of dimples arranged on the surface ofthe cover in each example are shown in Table 4. FIGS. 1 and 2 showvarious arrangements of dimples of sets A to C given in Table 4.

Table 5 presents the characteristics of the respective golf ballsobtained in these examples.

TABLE 1 Core Comparative Ingredients Example Example (parts by weight) 12 3 1 2 3 Base rubber HCBN-13 100 100 100 BR01 50 50 50 BR11 50 50 50Organic Perhexa 3M-40 0.3 0.3 0.3 0.6 0.6 0.6 peroxide Percumil D 0.30.3 0.3 0.6 0.6 0.6 Unsaturated Zinc acrylate 21.3 21.3 18.2 20.0 20.026.5 carboxylic acid metal salt Organic Zinc salt of 1.0 1.0 1.0 1.0 1.01.0 sulfur pentachloro- compound thiophenol Inorganic Zinc oxide 31.731.7 32.9 32.2 32.2 29.7 filler Antioxidant Nocrac NS-6 0.1 0.1 0.1 0.10.1 0.1

HCBN-13:

Produced by JSR Corporation. Cis-1,4 content, 96%. Mooney viscosity(ML₁₊₄ (100° C.)), 53. Polydispersity Mw/Mn, 3.2. Catalyst, neodymium.

BR01:

Produced by JSR Corporation. Cis-1,4 content, 96%. Mooney viscosity(ML₁₊₄ (100° C.)), 44. Polydispersity Mw/Mn, 4.2. Catalyst, nickel.Solution viscosity, 150 mPa.s.

BR11:

Produced by JSR Corporation. Cis-1,4 content, 96%. Mooney viscosity(ML₁₊₄ (100° C.)), 44. Polydispersity Mw/Mn, 4.1. Catalyst, nickel.Solution viscosity, 270 mPa.s.

Perhexa 3M-40:

Produced by NOF Corporation. Perhexa 3M-40 is a 40% dilution. The amountof addition indicated is the effective weight of the1,1-bis(t-butylperoxy)-3,3,5-trimethylcyclohexane added.

Percumil D:

Produced by NOF Corporation. Dicumyl peroxide.

Zinc Acrylate:

Produced by Nihon Joryu Kogyo K. K.

Zinc Salt of Pentachlorothiophenol:

Produced by Tokyo Kasei Kogyo Co., Ltd.

Zinc Oxide:

Produced by Sakai Chemical Industry Co., Ltd.

Nocrac NS-6:

2,2′-Methylenebis(4-methyl-6-t-butylphenol) produced by Ouchi ShinkoChemical Industry Co., Ltd.

TABLE 2 Mantle Ingredients Example Comparative Example (parts by weight)1 2 3 1 2 3 Himilan 1601 65 65 65 65 Surlyn 8120 75 75 Dynaron 6100P 2535 35 25 35 35 Behenic acid 20 20 20 Calcium hydroxide 2.2 2.2 2.2

Himilan 1601:

A sodium ion-neutralized ethylene/methacrylic acid copolymer ionomerproduced by DuPont-Mitsui Polychemicals Co., Ltd.

Surlyn 8120:

An ionomer resin produced by E.I. DuPont de Nemours and Company.

Dynaron 6100P:

A crystalline olefin block-bearing block copolymer produced by JSRCorporation.

Behenic acid:

Produced by NOF Corporation.

TABLE 3 Cover Ingredients Example Comparative Example (parts by weight)1 2 3 1 2 3 Himilan 1605 45 40 45 Himilan 1706 45 40 45 HSB 1561 10 2010 Himilan 1557 52 Himilan 1601 48 Surlyn 7930 60 60 Surlyn 6320 35 35Nucrel 9-1 5 5 Titanium dioxide 2 2 2 2 2 2

Himilan 1605:

A sodium ion-neutralized ethylene/methacrylic acid copolymer ionomerproduced by DuPont-Mitsui Polychemicals Co., Ltd.

Himilan 1706:

A zinc ion-neutralized ethylene/methacrylic acid copolymer ionomerproduced by DuPont-Mitsui Polychemicals Co., Ltd.

HSB 1561:

An amino-terminated block copolymer. This is a Cs-EB-Co typehydrogenated triblock polymer obtained by modifying the ends of thestyrene blocks with amino groups.

Himilan 1557:

A zinc ion-neutralized ethylene/methacrylic acid copolymer ionomerproduced by DuPont-Mitsui Polychemicals Co., Ltd.

Himilan 1601:

A sodium ion-neutralized ethylene/methacrylic acid copolymer ionomerproduced by DuPont-Mitsui Polychemicals Co., Ltd.

Surlyn 7930:

An ionomer resin produced by E.I. DuPont de Nemours and Company.

Surlyn 6320:

An ionomer resin produced by E.I. DuPont de Nemours and Company.

Nucrel 9-1:

A ternary acid copolymer produced by E.I. DuPont de Nemours and Company.

TABLE 4 Dimple Set A B C Total number of dimples 432 398 432 VR (%) 0.810.92 1.03 SR (%) 78.6 74.5 78.6 Number of differing types of dimples 3 43 Dimple 1 Diameter 3.9 4.1 3.9 Depth 0.16 0.19 0.2 Number 300 48 300Dimple 2 Diameter 3.4 3.8 3.4 Depth 0.13 0.18 0.17 Number 60 254 60Dimple 3 Diameter 2.6 3.2 2.6 Depth 0.10 0.16 0.14 Number 72 72 72Dimple 4 Diameter 2.4 Depth 0.12 Number 24

VR:

The ratio in percent of the sum of the individual spatial volumes foreach dimple below a planar surface circumscribed by an edge of thedimple to the total volume of a hypothetical sphere represented by thesurface of the golf ball were it to have no dimples.

SR:

The ratio in percent of the sum of the individual surface areas for eachdimple circumscribed by a dimple edge on a hypothetical sphere were thegolf ball to have no dimples to the surface area of the hypotheticalsphere.

TABLE 5 Ingredients Example Comparative Example (parts by weight) 1 2 31 2 3 Core Diameter (mm) 36.4 36.4 36.4 36.4 36.4 36.4 Hardness (m) 4.84.8 5.3 4.8 4.8 3.5 Mantle Thickness (mm) 1.65 1.65 1.65 1.65 1.65 1.65Hardness 51.0 53.0 53.0 51.0 53.0 53.0 Cover Thickness (mm) 1.5 1.5 1.51.5 1.5 1.5 Hardness 60 57 60 60 57 57 Dimple set A A B A C A BallDiameter (mm) 42.7 42.7 42.7 42.7 42.7 42.7 characteristics weight (g)45.3 45.3 45.3 45.3 45.3 45.3 Hardness (mm) 3.7 3.7 3.9 3.7 3.7 2.8Flight Initial velocity (m/s) 58.5 58.5 58.4 57.8 57.9 58.4 PerformanceSpin (rpm) 2600 2650 2570 2620 2640 3000 Carry (m) 183.5 184.0 183.0179.5 175.0 183.5 Total distance (m) 211.5 210.0 211.0 206.5 203.5 207.0Feel Driver soft soft soft soft soft Hard Putter soft soft soft softsoft Hard Scuff resistance OK OK OK OK OK NG

Core Diameter (mm):

The average of measurements taken at five different places on thesurface of the core.

Core Hardness (mm):

The deflection of the core when subjected to a load of 980 N (100 kgf).

Mantle Thickness (mm):

Calculated as

[(diameter of mantle-covered core)−(core diameter)]+2.

Mantle Hardness: Shore D hardness, as measured in accordance with ASTMD-2240.

Cover Thickness (mm):

Calculated as

[(ball diameter)−(diameter of mantle-covered core)]+2.

Cover Hardness:

Shore D hardness, as measured in accordance with ASTM D-2240.

Ball Diameter (mm):

The average of measurements taken at five different non-dimple places.

Ball Hardness (mm):

The deflection of the ball when subjected to a load of 980 N (100 kgf).

Flight Performance:

The initial velocity, spin rate, carry and total distance for each golfball were measured when the ball was struck at a head speed of 40 m/swith a driver (W#1) mounted on a swing machine made by Miyamae Co., Ltd.

Feel:

The feel of each ball when hit with a driver (W#1) and a putter wasrated by five top-caliber amateur golfers as “Soft,” “Ordinary,” or“Hard”. The rating assigned most often to a particular ball was used asthat ball's overall rating.

Scuff Resistance:

The ball was temperature conditioned to 23° C., then hit at a head speedof 33 m/s with a pitching wedge mounted on a swing machine. After beinghit, the ball was examined visually for signs of damage. The scuffresistance was rated as follows.

OK: Damage was not observed, or was of such a limited degree as to poseno impediment to further use of the ball.

NG: Considerable damage, such as surface scuffing and loss of dimples.

As described above and demonstrated in the foregoing examples, themulti-piece solid golf balls of this invention have a combination ofoutstanding flight performance, excellent scuff resistance and soft feelon impact that is unprecedented.

Japanese Patent Application No. 2002-349203 is incorporated herein byreference.

Although some preferred embodiments have been described, manymodifications and variations may be made thereto in light of the aboveteachings. It is therefore to be understood that the invention may bepracticed otherwise than as specifically described without departingfrom the scope of the appended claims.

What is claimed is:
 1. A multi-piece solid golf ball comprising a solidcore, a mantle of at least one layer, and a cover, wherein the solidcore is made of a rubber composition comprising (A) 100 parts by weightof a base rubber that contains 60 to 100 wt % of a polybutadiene of atleast 60% cis-1,4 structure and synthesized using a rare-earth catalyst,(B) 0.1 to 0.8 part by weight of an organic peroxide, (C) an unsaturatedcarboxylic acid or an unsaturated carboxylic acid metal salt or both,(D) an organic sulfur compound and (E) an inorganic filler, has adeflection when subjected to a load of 980 N (100 kgf) of 3.0 to 6.0 mm,and has a diameter of 30 to 40 mm; the mantle of at least one layer ismade of a thermoplastic resin composition, has a thickness per layer of0.5 to 2.0 mm, and includes an outermost layer which is in contact withthe cover and has a Shore D hardness of 20 to 60; the cover is composedprimarily of a mixture of (M) an amino-terminated block polymer and (N)an ionomer resin in a weight ratio M/N of 3/97 to 60/40, has a thicknessof 0.5 to 2.5 mm and a Shore D hardness of 50 to 70, and satisfies thecondition (Shore D hardness of mantle outermost layer)≦(Shore D hardnessof cover); and the golf ball has a deflection when subjected to a loadof 980 N (100 kgf) of 3.0 to 5.0 mm.
 2. The golf ball of claim 1,wherein the polybutadiene is a modified polybutadiene prepared bysynthesis using a neodymium catalyst, followed by reaction with aterminal modifier.
 3. The golf ball of claim 1, wherein the rubbercomposition includes: (A) 100 parts by weight of a base rubbercontaining 60 to 100 wt % of a polybutadiene of at least 60% cis-1,4structure and synthesized using a rare-earth catalyst, (B) at least twokinds of organic peroxide, (C) 10 to 60 parts by weight of anunsaturated carboxylic acid or an unsaturated carboxylic acid metal saltor both, (D) 0.1 to 5 parts by weight of an organic sulfur compound, and(E) 5 to 80 parts by weight of an inorganic filler.
 4. The golf ball ofclaim 1, wherein the thermoplastic resin composition comprises: 100parts by weight of resin components which include a base resin of (P) anolefin/unsaturated carboxylic acid binary random copolymer or a metalion neutralization product of an olefin/unsaturated carboxylic acidbinary random copolymer or both in admixture with (Q) anolefin/unsaturated carboxylic acid/unsaturated carboxylic acid esterternary random copolymer or a metal ion neutralization product of anolefin/unsaturated carboxylic acid/unsaturated carboxylic acid esterternary random copolymer or both in a weight ratio P/Q of 100:0 to25:75, and (R) a non-ionomeric thermoplastic elastomer in a weight ratio(P+Q)/R of 100:0 to 50:50; (S) 5 to 80 parts by weight of a fatty acidor fatty acid derivative having a molecular weight of 280 to 1,500, orboth; and (T) 0.1 to 10 parts by weight of a basic inorganic metalcompound capable of neutralizing un-neutralized acid groups in the baseresin and component S.
 5. The golf ball of claim 1, wherein the mantleconsists of an inner layer and an outer layer.
 6. The golf ball of claim1 wherein the cover bears on a surface thereof a plurality of dimples,each dimple having a spatial volume below a planar surface circumscribedby an edge of the dimple and having a surface area circumscribed by thedimple edge on a hypothetical sphere represented by the surface of thegolf ball cover were it to have no dimples; which golf ball has a dimplevolume occupancy VR, defined as the ratio of the sum of the individualdimple volumes to the volume of the hypothetical sphere, of 0.70 to1.00%, and a dimple surface coverage SR, defined as the ratio of the sumof the individual dimple surface areas to the surface area of thehypothetical sphere, of 70 to 85%.